FLIGHT NAVIGATION GUIDANCE CONTROL

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MAKING ADVANCED TECHNOLOGY WORK NORTHROP GRUMMAN CORPORATION 1840 Century Park East, 15th Floor Los Angeles CA 900672199 FLIGHT NAVIGATION GUIDANCE AND CONTROL SYSTEMS AND COMPONENTS THEREOF, COMPRISING, IN WHOLE OR IN PART, INTEGRATED INERTIAL AND GLOBAL POSITIONING NAVIGATIONAL APPARATUS, ASTRO/INERTIAL GUIDANCE APPARATUS, INERTIAL SENSORS, ACCELEROMETERS, GYROSCOPES, STRAP DOWN GYROS, MICRO-OPTIC GYROSCOPES, RING LASER GYROS, AND TESTERS THEREFOR, STANDARD ATTITUDE HEADING & REFERENCE SETS (SAHRS); FLIGHT AVIONIC SYSTEMS COMPRISING, IN WHOLE OR IN PART, COMPUTERS, COMPUTER PROGRAMS AND INSTRUCTION MANUALS PROVIDED THEREWITH, CONTROLS, AND VIDEO DISPLAYS THEREFOR; GROUND BASED NAVIGATIONAL SYSTEMS, NAVIGATIONAL AIDS AND COMPONENTS THEREOF, NAMELY, [ INSTRUMENT LANDING SYSTEMS (ILS), MICROWAVE LANDING SYSTEMS (MLS), VERY-HIGH-FREQUENCY OMNI-RANGE TACTICAL AIR NAVIGATION APPARATUS (VORTAC), DISTANCE MEASURING APPARATUS (DME), LOCALIZER, GLIDESLOPE, VERY-HIGH-FREQUENCY OMNI-DIRECTIONAL RANGE/DISTANCE MEASURING APPARATUS (VOR/DME), PRECISION DISTANCE MEASURING APPARATUS (P-DME), DOPPLER VERY-HIGH-FREQUENCY OMNI-DIRECTIONAL RANGE-FINDING APPARATUS (DVOR), NON-DIRECTIONAL BEACONS (NDB), ] REMOTE MAINTENANCE MONITORS (RMM), AND REMOTE MONITORING AND DIAGNOSTIC TESTERS THEREFOR; REMOTELY CONTROLLED AERIAL TARGETS, AND STRUCTURAL PARTS, AND DIAGNOSTIC TESTERS THEREFOR; AERIAL TARGET AND TACTICAL SUPPORT SYSTEMS COMPRISED OF REMOTE CONTROLS, RADAR, AND DIAGNOSTIC TESTERS THEREFOR; ELECTRONIC AUGMENTATION APPARATUS FOR USE ON TARGETS FOR PROVIDING SIMULATED EMISSION SIGNATURES OF THREAT AIRCRAFT; MISSILE/SHELL MISS-DISTANCE SCORING UNITS; ALTIMETERS; TACTICAL AID TO NAVIGATION GUIDANCE UNITS; ELECTRONIC UNITS FOR TRACKING AND DESIGNATING TARGETS; LASER DESIGNATORS AND RANGEFINDERS; LASER RADAR; ELECTRO-MECHANICAL AND ELECTRONIC APPARATUS FOR AIRCRAFT STORES MANAGEMENT; DIAGNOSTIC TESTERS AND APPARATUS FOR MONITORING AIRCRAFT STRUCTURES, ENGINES AND COMPONENTS; ELECTRONIC, VISUAL, INFRARED, AND ULTRAVIOLET COUNTER-MEASURES APPARATUS FOR WARFARE AND THREAT WARNING, AND DIAGNOSTIC TESTERS THEREFOR; MICROWAVE AND MILLIMETER-WAVE OSCILLATOR AND AMPLIFIER TUBES; RADAR SYSTEM MONITORS; CAMERAS AND OPTICAL ELEMENTS FOR USE IN THE VISUAL, INFRARED, AND ULTRAVIOLET COMPRISING COMPONENTS, MIRRORS, AND LENSES MADE WITH THIN FILM OPTICAL COATINGS; INFRARED IMAGERS AND DETECTORS AND PARTS THEREFOR; ELECTRO-OPTICAL AND INFRARED SENSORS AND SIGNAL PROCESSORS THEREFOR, FOCAL PLANE ARRAYS, FORWARD LOOKING INFRARED SENSORS (FLIR); LASERS AND LASER COMMUNICATIONS APPARATUS; COMPUTERS, COMPUTER PROGRAMS, AND INSTRUCTION MANUALS PROVIDED THEREWITH AND VIDEO DISPLAY UNITS, HIGH SPEED DATA LINKS, IMBEDDED PROCESSORS FOR COMPUTERS FOR INERTIAL NAVIGATION, COMPUTER PROGRAMS FOR IMAGE PROCESSING; RADIATION HARDENED ELECTRONIC CIRCUITS; GROUND SUPPORT APPARATUS FOR AIRCRAFT, NAMELY, FUEL SYSTEM TESTERS, JET ENGINE TESTERS, HYDRAULIC SYSTEM TESTERS, AIRCRAFT PART ALIGNMENT AND INSTALLATION FIXTURES;AERIAL TARGET LAUNCHERS AND TARGET TOW REELS;
NORTHROP NORTHROP CORPORATION Los Angeles CA FLIGHT NAVIGATION GUIDANCE AND CONTROL SYSTEMS AND COMPONENTS THEREOF, COMPRISING, IN WHOLE OR IN PART, INTEGRATED INERTIAL AND GLOBAL POSITIONING NAVIGATIONAL APPARATUS, ASTRO/INERTIAL GUIDANCE APPARATUS, INERTIAL SENSORS, ACCELEROMETERS, GYROSCOPES, STRAP DOWN GYROS, MICRO-OPTIC GYROSCOPES, RING LASER GYROS, AND TESTERS THEREFOR, STANDARD ATTITUDE HEADING AND REFERENCE SETS; FLIGHT AVIONIC SYSTEMS COMPRISING, IN WHOLE OR IN PART, COMPUTERS, COMPUTER PROGRAMS AND INSTRUCTION MANUALS PROVIDED THEREWITH, CONTROLS, AND VIDEO DISPLAYS THEREFOR; GROUND BASED NAVIGATIONAL SYSTEMS, NAVIGATIONAL AIDS AND COMPONENTS THEREOF, NAMELY, INSTRUMENT LANDING SYSTEMS, MICROWAVE LANDING SYSTEMS, VERY-HIGH-FREQUENCY OMNI-RANGE TACTICAL AIR NAVIGATION APPARATUS, DISTANCE MEASURING APPARATUS, LOCALIZER, GLIDESLOPE, VERY-HIGH-FRENQUENCY OMNI-DIRECTIONAL RANGE/DISTANCE MEASURING APPARATUS, PRECISION DISTANCE MEASURING APPARATUS, VERY-HIGH-FREQUENCY OMNI-DIRECTIONAL RANGE-FINDING APPARATUS, NON-DIRECTIONAL BEACONS, REMOTE MAINTENANCE MONITORS, AND REMOTE MONITORING AND DIAGNOSTIC TESTERS THEREFOR; REMOTELY CONTROLLED AERIAL TARGETS AND STRUCTURAL PARTS, AND DIAGNOSTIC TESTERS THEREFOR; AERIAL TARGET AND TACTICAL SYSTEMS COMPRISING, IN WHOLE OR IN PART, REMOTE CONTROLS, RADAR, AND DIAGNOSTIC TESTERS THEREFOR; ELECTRONIC AUGMENTATION APPARATUS FOR USE ON TARGETS FOR PROVIDING SIMULATED EMISSION SIGNATURES OF THREAT AIRCRAFT; MISSILE/SHELL MISS-DISTANCE SCORING UNITS; ALTIMETERS; TACTICAL AID TO NAVIGATION GUIDANCE UNITS; ELECTRONIC UNITS FOR TRACKING AND DESIGNATING TARGETS; LASER DESIGNATORS AND RANGEFINDERS; LASER RADAR; ELECTRO-MECHANICAL AND ELECTRONIC APPARATUS FOR AIRCRAFT STORES MANAGEMENT; DIAGNOSTIC TESTERS AND APPARATUS FOR MONITORING AIRCRAFT STRUCTURES, ENGINES AND COMPONENTS; AIRBORNE ELECTRONIC, VISUAL, INFRARED, AND ULTRAVIOLET COUNTERMEASURES APPARATUS FOR WAREFARE AND THREAT WARNING, AND DIAGNOSTIC TESTERS THEREFOR; MICROWARE AND MILLIMETER-WAVE OSCILLATOR AND AMPLIFIER TUBES; RADAR SYSTEM MONITORS; CARERAS AND OPTICAL ELEMENTS FOR USE IN THE VISUAL, INFRARED, AND ULTRAVIOLET LIGHT SPECTRUMS COMPRISING COMPONENTS, MIRRORS AND LENSES MADE WITH THIN FILM OPTICAL COATINGS; INFRARED IMAGERS AND DETECTORS AND PARTS THEREFOR; ELECTRO-OPTICAL AND INFRARED SENSORS AND SIGNAL PROCESSORS THEREFOR, FOCAL PLANE ARRAYS, FORWARD LOOKING INFRARED SENSORS; LASERS AND LASER COMMUNICATIONS APPARATUS; COMPUTERS, COMPUTER PROGRAMS, AND INSTRUCTION MANUALS PROVIDED THEREWITH; VIDEO DISPLAY UNITS, HIGH SPEED DATA LINKS, IMBEDDED PROCESSORS FOR COMPUTERS FOR INERTIAL NAVIGATION, COMPUTER PROGRAMS FOR IMAGE PROCESSING; RADIATION-HARDENED ELECTRONIC CIRCUITS; GROUND SUPPORT APPARATUS FOR AIRCRAFT, NAMELY, FUEL SYSTEM TESTERS, JET ENGINE TESTERS, HYDRAULIC SYSTEM TESTERS, AIRCRAFT PART ALIGNMENT AND INSTALLATION FIXTURES;AERIAL TARGET LAUNCHERS AND TARGET TOW REELS;
 

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Technical Examples
  1. The device (1) for guiding an aircraft at least over an intermediate trajectory between a first flight trajectory for a low-altitude flight and a second flight trajectory which starts at an initial point, and from which trajectory a parachute drop is carried out, comprises means (9) for determining a point of transition which lies on the first flight trajectory which represents the start of the intermediate trajectory, and which corresponds to the point where the aircraft must exit the first flight trajectory so as to reach the initial point under predetermined flight conditions, and means (13A, 13B) which use the point of transition to aid the guidance of the aircraft between the first and second flight trajectories.